Tree trimming apparatus and method

ABSTRACT

An apparatus and method for removing the tops of trees, the apparatus including a rotatable first boom configured for coupling to and extending vertically downward from an aircraft and a cutting assembly hingedly coupled to a bottom end portion of the first boom. The cutting assembly includes a housing containing a motor, the housing having an upper portion coupled to the bottom end portion of the first boom. A second boom extends from a lower portion of the housing and supports thereon a singular circular saw which is operatively coupled to the motor. The second boom is arranged at an angle of about 30° to about 55° relative to the first boom. This accomplished by including bend within the housing.

RELATED APPLICATIONS

This application is a continuation of U.S. application Ser. No.15/019,432, titled, “Tree Trimming Apparatus and Method,” and filed onFeb. 9, 2016, the entire contents of which are incorporated herein byreference.

FIELD OF THE INVENTION

The present invention is directed to an apparatus and method fortrimming vegetation, and more particularly, to a method for removing thetops of trees by cutting the tree tops with a saw suspended from anaircraft.

BACKGROUND OF THE INVENTION

Aerial saws for trimming vegetation are known in the art. For example,U.S. Pat. No. 4,554,781 discloses a tree trimmer apparatus including aboom hanging vertically downward from a helicopter and carrying aplurality of circular saws arranged with their blades nearly adjacentover a length of the boom. The boom is attached to the helicopter in amanner that prevents rotation about a vertical axis while allowingrotational movement about a horizontal axis at right angles to thenormal direction of motion of the helicopter. The blades are powered bya hydraulic motor with hydraulic fluid under pressure from a pump in thehelicopter.

U.S. Pat. No. 4,815,263 discloses an airborne tree trimming apparatusincluding a boom extension vertically suspended from a helicopter and aplurality of circular saw blades arranged in a tandem, coplanarrelationship on an operating boom which is attached to the boomextension by means of a boom pivot. The circular saw blades rotate aboutparallel, substantially horizontal axes which are oriented substantiallyat right angles to the normal direction of motion of the helicopter andare belt-driven by an internal combustion engine which is mounted on theoperating boom, above the circular saw blades.

U.S. Pat. No. 5,961,070 discloses an aerial chain saw suspended from ahelicopter by a non-rigid suspension system. A continuous chain extendsaround a chain saw bar, driven by a sprocket. Hydraulic lines to andfrom the helicopter provide hydraulic power to a hydraulic motor mountedat the upper end of the bar.

SUMMARY OF THE INVENTION

The present invention is directed to an apparatus and method forremoving the tops of trees with a saw suspended from an aircraft.According to one aspect of the invention there is provided a treetrimming apparatus including a rotatable first boom configured forcoupling to and extending vertically downward from an aircraft and acutting assembly hingedly coupled to a bottom end portion of the firstboom. The cutting assembly includes a housing containing a motor, thehousing having an upper portion coupled to the bottom end portion of thefirst boom. A second boom extends from a lower portion of the housingand supports thereon a circular saw which is operatively coupled to themotor. The second boom is arranged at an angle of about 30° to about 55°relative to the first boom. This accomplished by including bend withinthe housing. In particular, the housing includes a front wall, a rearwall and opposing lateral walls connecting the front and rear wallstogether, the front and rear walls each including a bend forming anangle of about 30° to about 55°.

In use, the apparatus is suspended from a helicopter and transported toa tree to be trimmed. When in transit, the first boom is maintained in afirst position with the second boom extending away from a forwarddirection of travel of the helicopter. This arrangement is moreaerodynamic than having the second boom extending laterally or forwardrelative to the direction of travel of the helicopter. As the helicopterapproaches the tree, the first boom is rotated into a second positionwith the second boom extending laterally from the forward direction oftravel of the helicopter. This arrangement of the second boom allows thehelicopter pilot to more easily view the tree to be trimmed andengagement of the circular saw with the tree than if the second boomextended toward the front or rear of the helicopter. As the apparatus ismoved towards the tree, a bottom end portion of the second boom, whichextend below a lower edge of the circular saw is used to guide the sawtowards the tree top so that the saw may engage and cut the tree top.

According to another aspect of the invention there is provided a treetrimming apparatus including a first boom portion extending verticallydownward from a helicopter, a second boom portion coupled to andsuspended from the first boom portion, the second boom portion beingarranged at about a 40° angle to about a 50° angle to the first boomportion, and a cutting member supported by the second boom portion. Ahousing containing a power source operatively coupled to the cuttingmember is coupled to and between the first boom portion and the secondboom portion. In particular, a hinge joint operatively couples the firstboom portion to the housing, which in turn, is rigidly coupled to thesecond boom portion.

According to yet another aspect of the invention, there is provided atree trimming apparatus including a flexible first boom rotatablycoupled to and extending vertically downward from an aircraft, housingcontaining a fuel tank and a motor operatively coupled to the fuel tank,the housing having an upper portion hingedly coupled to the bottom endportion of the first boom, a rigid second boom rigidly coupled to andextending downwardly from the housing, and a circular saw operativelycoupled to the motor and supported by the second boom. To assist theaircraft pilot with engaging the tree top and preventing pinching of thesaw blade as it cuts through a tree top, the second boom is arranged atan angle of about 45° relative to the first boom and includes a guideportion extending below a lower edge of the circular saw. In use, theapparatus is positioned above a tree and the guide portion of the secondboom is engaged with a tree top for guiding the circular saw towards thetree top.

BRIEF DESCRIPTION OF THE DRAWINGS

The disclosure can be better understood with reference to the followingdrawings. The elements of the drawings are not necessarily to scalerelative to each other, emphasis instead being placed upon clearlyillustrating the principles of the disclosure. Furthermore, likereference numerals designate corresponding parts throughout the severalviews.

FIG. 1 depicts a tree trimming apparatus and method of using same inaccordance with the present invention.

FIG. 2 is a perspective view of a coupling between a first boom and acutting assembly of the tree trimming apparatus of FIG. 1.

FIG. 3 is an elevational view of a side of the apparatus of FIG. 1.

FIG. 4 is a top plan view of the tree trimming apparatus of FIG. 1.

FIG. 5 is a bottom plan view of the tree trimming apparatus of FIG. 1.

FIG. 6 is a section view of the tree trimming apparatus of FIG. 1.

FIG. 7 depicts a guide portion of the tree trimming apparatus of FIG. 1engaging a tree for cutting.

FIG. 8 depicts the tree trimming apparatus of FIG. 7 cutting the tree.

DETAILED DESCRIPTION OF THE DRAWINGS

The present invention is directed to a tree trimming system for cuttingor removing the tops of trees. As depicted in FIG. 1, the systemgenerally includes an aircraft such as a helicopter 10, a first boom 12coupled to and extending vertically underneath helicopter 10 and acutting assembly 14, the cutting assembly consisting of a motor housing16, a second boom 18 and a circular saw 20, the circular saw and thesecond boom being arranged at a desired angle relative to first boom 12.In use, helicopter 10 is positioned over a tree 11 with first boom 12rotated so that second boom 18 extends laterally relative to helicopter10. As cutting assembly 14 is moved towards tree 11, a guide portion 22formed by a bottom end portion of second boom 18 is used by thehelicopter pilot to guide saw 20 towards the tree top so that the sawmay engage and cut the tree top.

Referring to FIG. 1, the underside of helicopter 10 is fitted with ahook motor 24 having a rotatable shaft extending downwardly therefromand terminating in a hook 26. Suspended from hook 26 is first boom 12.First boom 12 may be constructed from a fifty foot, approximately threeinch diameter aluminum pipe. The length of first boom 12 can be greater,for example, if the tree tops to be cut are adjacent to structures thatare taller than the trees such as power lines or towers. Rigidly coupledto the upper end of first boom 12 is a loop 28 through which hook 26 issecured. The attachment of loop 28 to hook 26 allows the pilot toselectively rotate first boom 12 in either direction by remotelyactivating hook motor 24. It is contemplated that a redundant hookingsystem may be used to secure and suspend first boom 12 from helicopter10. Such a system may include, in addition to hook 26, a chain coupledto and been first boom 12 and helicopter 10 or hook 26. It is alsocontemplated that a hooking system may be implemented giving the pilotthe option of remotely releasing first boom 12 from helicopter 10 in anemergency, for example, if saw 20 or guide portion 22 becomes entangledin a tree or power line. Such a system may include means for detachinghook motor 24 from the underside of helicopter 10 or releasing hook 26from hook motor 24.

Referring to FIG. 2, located at the bottom end of first boom 12 is abracket 30 rigidly coupled thereto. Bracket 30 is configured forhingedly coupling first boom 12 to cutting assembly 14. Bracket 30includes opposing arms 32 which, in part, define a slot 34. Integrallyformed with the top end of motor cage 14 is a cylinder 36. Cylinder 36is configured for being received within slot 30 and secured betweenopposing arms 32 by a pin 38. In particular, pin 38 extends to andbetween opposing arms 32 and is securely fixed there between. Arrangedin this manner, cylinder 36 and cutting assembly 14 are free to rotateabout pin 38.

As illustrated in FIG. 2, the rotational axis defined by rotation ofcylinder 36 about pin 38 is not arranged perpendicularly to therotational axis of first boom 12. Rather, the rotational axes are tiltedrelative to one another. As explained below, the angle formed by theintersection of rotational axes about pin 38 and first boom 12, incombination with the design of motor cage 14, ensures that a planeformed by saw 20 intersects first boom 12 or the rotational axis thereofat about a 135° angle. This way, when in use, saw 20 can engage avertically extending branch or top of tree 11 at an angle of about 45°,which increases the cutting efficiency of the saw 20 while decreasingpinching of saw 20 by the vertically extending portion of the treeduring cutting.

More particularly, as depicted in FIGS. 2 through 5, motor cage 16includes a first wall 40 forming a first face, a second wall 42 forminga second face and a pair of opposing side walls coupling first andsecond walls 40, 42 together to form an enclosure. The enclosure has anupper portion 44 having a generally conical or pyramid shape terminatingat the upper end thereof at cylinder 36, a middle portion 46 having agenerally rectangular shape and a lower portion 48 having a generallyhalf-conical or half-pyramid shape. Upper portion 44 is arranged atangle relative to middle portion 46 with first and second walls 40, 42forming complimentary bends. The angles formed between the upper andmiddle portions 44, 46 by the bends, in combination with the angleformed between the rotational axes of first boom 12 and cylinder 36about pin 38, are configured to make sure saw 20 is maintained at anangle of about 45° relative to tree 11 during cutting.

Referring to FIGS. 3 through 5, the lower end of lower portion 48 ofmotor cage 16 terminates in a rectangular sleeve 50. Sleeve 50 definesan opening into which an upper end of second boom 18 is rigidly securedby bolts or the like. AS best illustrated in FIG. 3, first face of firstwall 4 is essentially coplanar with the face of second boom 18 fromwhich saw 20 extends. Second boom 18 is constructed of rectangular steeltubing having a length of about 11′. Located about 4 feet from the lowerend of second boom is a saw connection bracket 52 for rotatably securingsaw 20 to second boom 18. That portion of the lower end of second boom18 that extends downwardly from a periphery 21 of saw 20 is referred toas the guide portion 22.

Referring to FIG. 6, saw 20 is operatively coupled to a saw motor 54contained within motor cage 16 by a continuous belt 56. Belt 56 engagesa wheel that is rotatably coupled to a drive shaft of the motor. Belt 56extends downwardly through hollow second boom 18 and engages a wheelthat is operatively coupled to a saw shaft 60. Upon rotation of sawshaft 60, saw 20 is caused to rotate. Fuel for saw motor 54 is stored intank 58, which is also contained within motor cage 16.

When in use, cutting assembly 14 is coupled to first boom 12 asdescribed above and suspended underneath helicopter 10. During transportto a worksite, first boom 12 is rotated such that second boom 18 isaligned with the forward direction of travel of the helicopter, with thesecond boom trailing behind motor cage 16. Trailing second boom 18behind motor cage 16 minimizes the amount of drag created by the cuttingassembly as it is moved through the air.

Referring to FIGS. 1, 7 and 8, once helicopter 10 reaches the worksite,the pilot remotely activates hook motor 24 and thereby rotates firstboom 12 90° so that second boom 18 extends out laterally relative to thehelicopter. This is done so that the pilot can see saw 20. The pilotthen remotely activates saw motor 54 causing saw 20 to rotate. The pilotmoves saw 20 towards tree 11 until guide portion 22 of second boom 18contacts tree 11. With guide portion 22 pressing against tree 11, thepilot moves saw 20 toward tree 11 so that saw 20 may engage and cut tree11. When engaged with tree 11, saw 20 will form an angle A of about 45°relative to tree 11 and an angle B of about 135° relative to first boom12. By engaging tree 11 at a 45° with saw 20, the tree is less likely topinch saw 20 and thereby hinder cutting than if saw 20 were arranged atabout a 90° angle to tree 11. Following cutting of tree 11, the pilotremotely deactivates saw motor 54 and activates hook motor 24 forrotating second boom 18 back into the transport position.

As will be understood by those familiar with the art, the presentinvention may be embodied in other specific forms without departing fromthe spirit or essential characteristics thereof. Accordingly, thedisclosures and description herein are intended to be illustrative, butnot limiting, of the scope of the invention which is set forth in thefollowing claims.

What is claimed is:
 1. A tree trimming apparatus comprising: a firstboom assembly suspended from and coupled at an upper end portion thereofto an aircraft, a cutting assembly coupled to a lower end portion of thefirst boom assembly, the cutting assembly including a housing containinga motor, a second boom assembly extending downward from a lower portionof the housing and at an angle relative to the first boom assembly, anda saw attached to the second boom assembly and operatively coupled tothe motor, wherein the second boom assembly extends laterally from thehousing relative to the aircraft a distance from the housing sufficientthat a pilot of the aircraft can view the saw when it engages with atree as the tree is trimmed and the housing extends laterally from thefirst boom assembly relative to the aircraft.
 2. The apparatus of claim1 wherein the angle is between 30° to 55°.
 3. The apparatus of claim 1wherein the housing includes a front wall, a rear wall and opposinglateral walls connecting the front and rear walls together, the frontwall including a bend forming an angle of 30° to 55°.
 4. The apparatusof claim 1 wherein the first boom assembly is rotatable relative to theaircraft and the second boom assembly is rigidly coupled to the housing.5. The apparatus of claim 1 wherein the second boom assembly includes aboom section extending away from the housing and below a lower edge ofthe saw.
 6. A tree trimming apparatus suspended underneath an aircraft,the apparatus comprising: a first boom coupled to the aircraft, a secondboom hingedly coupled and arranged at an angle to the first boom, and acircular saw supported on the second boom and operatively coupled to amotor, wherein the second boom extends laterally away from the firstboom relative to the aircraft a distance from the first boom sufficientthat a pilot of the aircraft can view the circular saw when it engageswith a tree as the tree is trimmed.
 7. The apparatus of claim 6 whereinthe motor is contained within a motor housing that extends laterallyfrom the first boom relative to the aircraft.
 8. The apparatus of claim7 wherein the motor housing includes a front wall, a rear wall andopposing lateral walls connecting the front and rear walls together, thefront wall including a bend forming an angle of 30° to 55°.
 9. Theapparatus of claim 7 wherein the first boom is rotatable relative to theaircraft and the second boom is rigidly coupled to the motor housing.10. The apparatus of claim 6 wherein the angle is between 30° and 55°.11. The apparatus of claim 6 wherein the second boom includes a boomsection extending away from the first boom and below a lower edge of thecircular saw.
 12. A tree trimming apparatus comprising: an assemblyincluding a first boom, a second boom having a longitudinal axis, amotor housing coupled to and between the first boom and the second boomand a saw supported on the second boom, wherein the first boom iscoupled to an aircraft and the assembly is suspended from the aircraftwith the longitudinal axis extending laterally relative to the aircraftand the second boom extends laterally relative to the aircraft adistance sufficient that the saw is viewable by a pilot in the aircraftwhen using the saw to cut off a top of the tree with the saw.
 13. Theapparatus of claim 12 wherein the first boom is arranged at an angle of30° to 55° relative to the second boom.
 14. The apparatus of claim 13wherein the motor housing includes a front wall, a rear wall andopposing lateral walls connecting the front and rear walls together, thefront wall including a bend forming an angle of 30° to 55°.
 15. Theapparatus of claim 12 wherein the first boom is rotatable relative tothe aircraft and the second boom is rigidly coupled to the motorhousing.
 16. The apparatus of claim 12 wherein the second boom includesa boom section extending away from the motor housing and below a loweredge of the saw.